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Photo: Mark L. Psiaki, Brady W. O’Hanlon, Steven P. Powell, Jahshan A. Bhatti, Todd E. Humphreys, and Andrew Schofield Spoofing Detection with Two-Antenna Differential Carrier Phase By Mark L. Psiaki, Brady W. O’Hanlon, Steven P. Powell, Jahshan A. Bhatti, Todd E. Humphreys, and Andrew Schofield A new method detects spoofing attacks that are resistant to standard RAIM technique and can sense an attack in a fraction of a second without external aiding. The signal-in-space properties used to detect spoofing are the relationships of the signal arrival directions to the vector that points from one antenna to the other. A real-time implementation succeeded against live-signal spoofing attacks aboard a superyacht, the White Rose of Drachs shown above, cruising in international waters. Read more about “Red Team, White Team, Blue Team” below. Concerns about spoofing of open-service GNSS signals inspired early work on simple receiver-autonomous integrity monitoring (RAIM) methods based on the consistency of the navigation solution. Work on new classes of defense techniques began in earnest after the demonstration of a powerful spoofer that is undetectfable by simple pseudorange-based RAIM methods. There has been a sense of urgency to solve the spoofing problem since the Iranians captured a classified U.S. drone in 2011 and made unsubstantiated claims to have spoofed its GPS. Two dramatic field demonstrations of the spoofer developed by author Humphreys and colleagues at the University of Texas, Austin, heightened interest in spoofing detection: one involved deception of a small airborne unmanned autonomous vehicle (UAV), causing it to dive towards the ground; another sent a superyacht off course without raising any alarms on its bridge. One class of spoofing detection methods uses encrypted signals, their known relationships to the open-service signals, and after-the-fact availability of encryption information. Such techniques require a high-bandwidth communication link between the potential victim of a spoofing attack and a trusted source of after-the-fact encryption information, and may involve significant latency between attack and detection. Another class of methods uses advanced RAIM-type techniques. Instead of considering only pseudorange consistency, these RAIM techniques examine additional signal characteristics such as absolute power levels, distortion of the PRN code correlation function along the early/late axis, the possible existence of multiple distinct correlation peaks in signal-acquisition-type calculations, and other signal or receiver characteristics. Such methods are relatively simple to implement because they do not require much additional hardware, if any, but some of these strategies can have trouble distinguishing between multipath and spoofing or between jamming and spoofing. A third class proposes the addition of Navigation Message Authentication bits. These are encrypted parts of the low-rate navigation data message. Such techniques require modification of the navigation data message and can allow long latencies between the onset of a spoofing attack and its detection. A fourth class exploits the differing signal-in-space geometry of spoofed signals in comparison to true GNSS signals. All spoofed signals typically arrive from the same direction, but true signals arrive from a multiplicity of directions. Some of these methods use receiver antenna motion to achieve direction-of-arrival sensitivity. Others use an array of two or more receiver antennas. The most powerful of these detection strategies exploit models of the effects on carrier-phase data of antenna motion or antenna-array geometry. This knowledge may be partial because an unknown antenna-array attitude may need to be determined as part of the detection calculation. Their power derives from the high degree of accuracy with which a typical GNSS receiver can measure beat carrier phase. Goals. This research follows on moving-antenna/carrier-phase-based spoofing detection work. One of our goals has been to remove the necessity for moving parts by using two antennas and processing their carrier-phase data. A second goal has been to achieve real-time operation. An earlier prototype moving-antenna system (see “GNSS Spoofing Detection,” GPS World, June 2013) used post-processing and completed its spoofing detection calculations days or weeks after the recording of wide-band RF data during live-signal attacks. A third goal has been to test this system against actual live-signal spoofing attacks to prove its real-time capabilities and evaluate its performance during the two phases of an attack: the initial signal capture and the post-capture drag-off to erroneous position and timing fixes. Two-Antenna System Architecture The system consists of two GNSS patch antennas, GPS receiver hardware and software, and spoofing detection signal-processing hardware and software. Figure 1 shows two versions. The left-hand version connects its two patch antennas to an RF switch. The single analog RF output of the switch is input to a GNSS receiver that is standard in all respects, except for two features. First, it controls the RF switch or, at least, has access to the switching times. Second, it employs a specialized phase-locked loop (PLL) that can track the beat carrier phase of a given signal through the phase jumps that occur at the switching times. The right-hand version connects each antenna to an independent GPS receiver, likely connected to a common reference oscillator. Figure 1. Two configurations:, the RF-switched-signal/single-receiver configuration (left) and the two-receiver configuration (right). The last element of each system is a spoofing detection signal-processing unit. Its inputs are the single-differenced beat carrier phases of all tracked signals, with differences taken between the two antennas. In the switched antenna system, each difference is deduced by the specialized PLL. In the two-receiver system, the single-differences are calculated explicitly from each receiver’s beat carrier-phase observables. Except for the final spoofing detection unit, the two-receiver system on the right-hand side of Figure 1 is already available commercially. Typical applications are CDGPS-based attitude/heading determination. Thus, this is the easiest version to implement. This system could include more than two antennas. A multi-antenna system could have a dedicated RF front-end and a dedicated set of receiver channels for each antenna, as on the right of Figure 1. Alternatively, a multi-antenna system could include an RF switch between any one of the multiple antennas at the command of the receiver. The latter design would entail a slight modification to the specialized PLL to track multiple independent phase jumps for the independent antenna switches. Principles. The principles used to detect spoofing can be understood by considering and comparing the signal-in-space and antenna geometries shown in Figure 2, the two-antenna system and three GNSS satellites for a typical non-spoofed case, and Figure 3, a spoofed case. The salient difference is that the different GNSS signals arrive from different directions for the non-spoofed case, namely and . They all arrive from the same direction, the direction of the spoofer , for the spoofed case. For detection purposes, the important geometric feature is the projection of each direction of arrival onto the known separation vector between the two antennas, bBA. This projection has a direct effect on the beat carrier-phase difference between the two antennas. In the non-spoofed case, this effect will vary between the different received signals in ways consistent with the attitude of the vector. In the spoofed case, all of these carrier-phase differences will be identical. The spoofing detection algorithm decides between two hypotheses about the carrier-phase differences, one conjecturing a diversity consistent with authentic signals and the other conjecturing the sameness that is characteristic of spoofed signals. Figure 2. Geometry of two-antenna spoofing detection system and GNSS satellites for non-spoofed case. Figure 3. Spoofed-case geometry of two-antenna spoofing detection system and GNSS spoofer. Hypothesis Test The PDF paper on which this article is based presents the non-spoofed and spoofed signal models that form the basis of a hypothesis test, develops optimal estimation algorithms that fit the observed differential beat carrier phases to the two models, and shows how these estimates and their associated fit error costs can be used to develop a sensible spoofing detection hypothesis test. Download the PDF here. Offline and Live-Signal Testing We tested a prototype version of the two-antenna system as depicted on the righthand side of Figure 1. The antennas connect to two independent RF front-ends that run off of the same reference oscillator. These RF front-ends provide input to two independent receivers that track each signal using a delay-lock loop (DLL) and a PLL. Figures 4 and 5 show system elements: two GPS patch antennas mounted on a single ground plane with a spacing of 0.14 meters, two RF front-ends — universal software radio peripherals (USRPs) — with a common ovenized crystal oscillator. Digital signal-processing functions are implemented in real-time software radio receivers (SWRX) running in parallel on a Linux laptop, written in C++. Spoofing detection calculations are performed on the same laptop using algorithms encoded in Matlab. Figure 4. The two antennas of the prototype spoofing detection system mounted on a common ground plane. Figure 5. Signal processing hardware of the prototype spoofing detection system. A key feature of this architecture is the ability of its real-time software radios’ C++ code to call the spoofing detector’s Matlab tic function and to pass carrier-phase and other relevant data to the tic function. This feature served to shorten the implementation and test cycle for the prototype system by eliminating the need to translate the original Matlab versions of the spoofing detection algorithms into C++. This enabled rapid re-tuning and redesign of the spoofing detection calculations, exploited during the course of live-signal testing. The Matlab package displays real-time signal authentication information. Figure 6 shows the version of the display used for this study’s culminating live-signal tests. All displays are updated in real time. The upper left, upper right, and lower left plots scroll along their horizontal time axes to keep the most recent 4.5 minutes of data available. The lower right compass updates each time a new spoofing detection calculation is performed. The green dots in the upper left plot indicate that the time between spoofing detections, Δtspf , is nominally 1 second, though sometimes the gap is longer due to lack of a sufficient number of validated single-differenced carrier phases to carry out the calculation. Thus, the nominal update time for all of the plots in this display is 1 second. Faster updates are possible with the Matlab software, but Δtspf was deemed sufficiently fast for this study’s experiments. The most important panel in Figure 6 is the upper left spoofing detection statistic time history. The magenta plus signs on the plot show the spoofing detection threshold chosen for this case, γth. The computed γ values are plotted as green o’s if they lie above γth and as red asterisks if they lie below. If γ is above γth, the message “GPS Signals Authenticated” is displayed on the plot; if below, the message switches to the spoofing alert: “GPS SPOOFING ATTACK DETECTED!” Figure 6. Spoofing detector real-time display. Clockwise from top left: the spoofing detection statistic time history γ(t); four diagnostic time histories that include time histories of the number of satellites used for spoofing detection L(t) (blue asterisks), their corresponding GDOP(t) values (magenta o’s), the time increment between spoofing detection tests Δtspf(t) (green dots), and the compass heading ψ(t) as determined from the two-antenna non-spoofed-case solution (black dots); Compass display; and time history of GPS PRN number availability. The other three panels proved helpful in diagnosing system performance. A low L value (near 4) or a high GDOP value in the upper right panel indicated poorer reliability of the spoofing detection calculations. A correct compass heading in the absence of spoofing provided a check on the system. During spoofing attacks, the compass heading became jumpy, thereby providing another possible indicator of inauthentic signals. The vertical scale of the lower left panel lists the possible GPS PRN numbers. The presence of a green or red dot at the level corresponding to a given PRN number indicates that one or both receivers is seeing something from that satellite at the corresponding time. If the dot is red, then the returned data are incomplete or are deemed to be insufficiently validated for use in the spoofing detection calculation. If the dot is green, then the data from that PRN have been used in the detection that has been carried out at that time. Another feature of the prototype spoofing detection system is its ability to record the wide-band RF data from its two antennas. For each spoofing scenario, the raw samples from both USRPs were recorded while the real-time software receiver was performing its signal-processing operations and while the real-time spoofing detector was doing its calculations. These recorded data streams will allow off-line analysis and testing of a re-tuned or completely redesigned spoofing detection system. Red Team Receiver/Spoofer. The UT Austin spoofer’s attack strategy overlays the spoofed signal on top of the true signals, ramps up the power to capture the receiver tracking loops, and finally drags the pseudorange, beat carrier phase, and carrier Doppler shift off from their true values to spoofed values. Figure 7 shows the pseudorange part of a spoofing attack: cross-correlation of the receiver’s PRN code replica with the total received signal (blue solid curve); the receiver’s early, prompt, and late correlations (red dots); and the spoofer signal (black dash-dotted curve). In the top plot, the spoofer has zero power, and the receiver sees only the true signal. The second and third plots show the spoofer ramping up its power while maintaining its false signal in alignment with the true signal. The spoofer power in the middle/third plot is sufficient to capture control of the three red dots of the receiver’s DLL. In the fourth and fifth plots, the spoofer initiates and continues a pseudorange drag-off, an intentional falsification of the pseudorange as measured by the victim receiver’s DLL. Figure 7. Receiver/spoofer attack sequence as viewed from a channel’s code offset cross-correlation function. Spoofer signal: black dash-dotted curve; sum of spoofer and true signals: blue solid curve; receiver early, prompt, and late correlation points: red dots. The spoofer performs drag-off simultaneously on all spoofed channels in a vector spoofing attack that maintains consistency of all spoofed pseudoranges. After the initiation of drag-off, the victim receiver computes a wrong position, a wrong true time, or both, but the residual pseudorange errors in its navigation solution remain small. Therefore, this type of attack is not detectable by traditional pseudorange-based RAIM calculations. The receiver spoofer hardware consists of a GNSS reception antenna, the receiver spoofer signal-processing unit, and the spoofer transmission antenna (Figure 8). Figure 8a. Receiver/spoofer hardware: GPS reception antenna on ship’s rear upper deck. Figure 8b. Receiver/spoofer hardware: directional transmission antenna pointed at the ship’s GPS antenna and the detector antenna pair near the defended ship’s antenna. The orientation of the spoofing transmission antenna, combined with its remote location from the receiver/spoofer’s reception antenna, ensured that the spoofer did not self-spoof. Figure 8c. Receiver/spoofer hardware: spoofer electronics, located amidships. The receiver/spoofer requires tuning of its transmission power levels. If the power is too high, its spoofing attacks will be too obvious. A very high transmitted power could also saturate the front-end electronics of the intended victim, causing it to jam the system rather than spoof it. If transmitted power is too low, it will not capture the victim’s tracking loops, and its spoofing attack will fail. The proper power level depends on the gain patterns of the spoofer transmission antenna and the victim receiver antenna and on their relative geometry. Attack Test Scenarios. Three sets of tests were conducted to develop and evaluate the spoofing detection system. The first tests started by recording wideband RF GPS L1 data using USRPs. These data were post-processed in two software receivers that recorded the outputs of their signal tracking loops. Afterwards, the Matlab spoofing detection calculations were run using the recorded tracking loop data as inputs. These preliminary tests at Cornell and Austin proved the efficacy of the spoofing detection algorithms. They did not, however, test system performance during the transition from non-spoofed to spoofed signals that takes place at the initiation of a spoofing attack. The second set of tests was carried out using the first real-time version of the system, after the Matlab spoofing detection calculations were repackaged into a tic function and linked to the C++ real-time software receivers. This set of tests also was unable to probe the system’s performance at the onset of a spoofing attack, before the signal drag-off. The final set of tests was conducted aboard the White Rose of Drachs in the Mediterranean’s international waters. The power adjustment tests on June 27 needed a means to decide whether a given attack had captured the tracking loops of the ship’s GPS receiver. The strategy for confirming capture was to perform a noticeable drag-off after the initial attack. We settled on a vertical drag-off as providing the most obvious indication of a successful capture. Successful attacks dragged the receiver’s reported altitude as high as 5,000 meters. The tests that evaluated spoofer and spoofing detector antenna placements relative to the ship’s GPS antenna were also important to achieving sensible results. Various placements were tried. The most successful relative geometry is depicted in Figure 8. The placement of the detector antennas relative to the defended antenna is atypical of likely real-world detection scenarios. It is expected that a real-world spoofing detector will be integral with the defended GNSS receiver. The culminating live-signal attack involved a 50-minute spoofing scenario in which the attacker took the ship — apparently — from the Adriatic to the coast off of Libya. The scenario’s long distance and short duration required a mid-course speed in excess of 900 knots. This spoofing scenario was designed in the simplest possible way, by taking a straight-line course in WGS-84 Cartesian coordinates from the true location to the spoofed location off of Libya. This course took the spoofed yacht position across the Italian and Sicilian land masses and below the Earth’s surface to a maximum depth of more than 23 kilometers. Obviously, the White Rose was physically unable to execute this maneuver. Its crew would not have needed spoofing detection to realize that its GPS receiver was returning false readings. The main points of this last test were to dramatize the potential errors that can be caused by a spoofer and to check whether the spoofing detector could continue to function under these drastic conditions. Figure 9 highlights this unusual scenario with two displays from the ship’s bridge, photographed during the attack. The GPS display shows the speed, 621 kn (knots), and the altitude, 7376 m. The chart display shows the yacht on (or rather, below) dry land and halfway across the “insole” of Italy’s boot. It also shows a tremendously long velocity vector, extending beyond the chart. Figure 9a. The ship’s bridge GPS receiver display during the Libya spoofing scenario. Figure 9b. The GPS-driven chart during the Libya spoofing scenario. Spoofing Detection Test Results Various signal output time histories (Figure 10) illustrate the attack sequence and suggest means to evaluate the spoofing detection system. The upper panel plots the fractional portions of the two-antenna spoofing detector’s single-differenced beat carrier-phase time histories, Δϕ1BA, …, ΔϕLBA for the L = 7 tracked PRN numbers 16, 18, 21, 22, 27, 29, and 31. The middle panel plots the amplitude time history of the 100 Hz prompt [I;Q] accumulation vector for PRN 16, as received at Antenna A of the detection system. The bottom panel plots the PRN 16 carrier Doppler shift time history. Figure 10. Indicators of initial capture and drag-off during Libya spoofing attack, as measured by the spoofing detection receiver. This was a strong attack in which the spoofer power was 10.7 dB higher than the power of the real signal for PRN 16. The other spoofed signals had power advantages over their corresponding true signals that ranged from 3.3 dB to 13.6 dB, and the spoofer’s mean power advantage was 10.4 dB. Therefore, the onset of the spoofing attack at 196.1 sec is clearly indicated by the sudden jump in (I2+Q2)0.5 on the middle panel. The upper panel shows a corresponding sudden coalescing of the single-differenced beat carrier phases, which implies that the spoofing detection algorithm should have been able to detect this attack. The spoofer drag-off started at 321.5 sec, as evidenced by the sudden change in the slope of the carrier Doppler shift time history on the lower panel. The period after the initial attack and before the drag-off is delimited by the vertical magenta and cyan dash-dotted lines. During this interval the spoofer waited to capture the receiver’s tracking loops. The single-differenced phase time histories in the upper plot appear somewhat noisier during the interim pre-drag-off period of the attack than after the start of the drag-off at 321.5 sec. The grey dotted curve for PRN 27 is an exception because it becomes noisy again starting at about 450 sec due to decreased signal power. The increased noisiness of the differential phase time histories during the interim period is probably the result of interference between the true and spoofed signals, which are likely beating slowly against each other. The response of the spoofing detection algorithm during this phase is uncertain because this multipath-like beating between the two signals is not modeled. Figure 11 demonstrates performance of the spoofing detection algorithm for the Libya attack scenario. The upper panel of the figures is a repeat of the upper panel of the single-differenced beat carrier-phase time histories from Figure 10, except that they are plotted for a longer duration. The lower panel shows the γ(t) spoofing detection statistic time history. It plots the same information that appeared in the upper left panel of Figure 6 during the corresponding real-time detection tests. At 196 sec γ(t) is clearly above the blue dash-dotted spoofing detection threshold γth. At 196.4 sec it is clearly below γth , which indicates a spoofing detection. It remains below γth for the duration of the attack. In this reprocessed version of the detection calculations, γ(t) has been updated at 5 Hz. Therefore, the earliest possible detection point would have been 196.2 sec, which is 0.1 sec after the onset of the attack. This point corresponds to the green dot in the lower panel of Figure 11 that lies slightly above the blue dash-dotted γth line. Theoretically, the system might have detected the attack at this time, but the finite bandwidth of the two receivers’ PLLs caused lags in the transitions of the single-differenced phases in the top plot, which led to the 0.3 sec lag in the detection of the attack. It is encouraging, however, that the spoofing detector worked well during the initial pre-drag-off phase of the attack, from 196.1 to 321.5 sec, despite the added noisiness of the single-differenced carrier phases in the top plot, likely caused by beating between the true and spoofed signals. Figure 11. Single-differenced carrier-phase time histories (top plot) and corresponding spoofing detection statistic time history (bottom plot) for Libya spoofing attack scenario. Figure 12 plots the same quantities as in Figure 11, but for a different spoofing attack, a little less overt than the Libya attack. The power advantage of the spoofer ranged from 3.0 to 14.0 dB for the different channels with a mean power advantage = 9.2 dB. It was detected by the system, as evidenced by the convergence of the single-differenced carrier phases at the onset of the attack at 397.5 sec. The spoofing detection statistic in the bottom panel dives near to the γth detection threshold at the onset of the attack and sometimes passes below it, but it does not stay permanently below the threshold until after the time of drag-off, after 531 sec. Figure 12. Single-differenced carrier phase time histories (top plot) and spoofing detection statistic time history (bottom plot) for a spoofing attack with a slightly lower power advantage than the Libya attack. The large oscillations of the single-differenced carrier phases during the pre-drag-off initial capture interval from 397.5 to 531 seconds is likely due to beating between the true and spoofed signals. The largest variations occur for PRNs 12 and 31, which are the ones with the lowest spoofer power advantages, 3.2 and 3.0 dB, respectively. Apparently these oscillations cause γ(t) sometimes to take on values slightly above γth during the interval 397.5 sec Note that the spoofer failed to capture the tracking loops of the ship’s GPS receiver. This is surprising, given the average spoofer power advantage of 9.2 dB above the true signals. We conjecture that the ship’s GPS antenna had lower gain in the low-elevation direction toward the spoofer transmission antenna than did the detector’s antennas. A lower gain would reduce the spoofer power advantage in the ship’s receiver and could explain why the spoofer failed to deceive it. Many additional spoofing attacks were carried out aboard the ship. The spoofing detector proved finicky. It took quite some time to get the spoofing detection two-antenna system positioned in a sensible place relative to the ship’s GPS antenna so as to be sensitive to nearly the same spoofing signals. In addition, the spoofing detector’s GPS receiver tended to lose lock at the initiation of an attack, prior to signal drag-off. This was likely caused by the large power swings of the received signals due to beating of the true signals against the spoofed signals. This problem went away at higher spoofer power levels. When lock was lost, the software receiver would attempt to re-acquire the signal. Often a reacquisition would succeed only after signal drag-off by the spoofer. Typically, the spoofing detector immediately detected the attack once it had reacquired the spoofed signals that were no longer beating against the true signals due to having been dragged sufficiently far away from them, as in Figure 7. Re-analysis of the recorded data indicated that poor PLL tuning may have caused the losses of lock during the initial attacks. Spoofing detection calculations carried out on the reprocessed data have proved more reliable when implemented with a better PLL tuning. Two attacks were carried out with only a subset of the visible GPS satellites being spoofed. The first involved spoofing 7 of 9 visible satellites, and the second test spoofed only 4 of 9. The spoofing detection system had trouble maintaining signal lock during the initial part of the first attack. It subsequently reacquired signals and was able to detect the attack successfully after reacquisition. The first attack also succeeded in capturing the ship receiver’s tracking loops as evidenced by spoofing of the yacht to climb off the sea surface. The second attack, with only four spoofed satellites, was not detected by the prototype system, but it succeeded in deceiving the ship’s GPS receiver about its altitude. This latter result indicates a need to modify the detection calculations to allow for the possibility of partial spoofing. In their current form, they assume that all signals are either spoofed or authentic. Of course, in the partial spoofing case it may also be possible to use traditional pseudorange-based RAIM techniques to detect an attack. Possible Future Work Directions The tests suggest further work on the following topics,which are discussed in more detail in the PDF paper on which this article is based: Improved detection during pre-drag-off initial phase of attack; Detection when only a subset of signals are spoofed; Advanced RAIM techniques; A real-time prototype of the switched-antenna version; Detection of a spoofer that uses multiple transmission antennas; Reacquisition of true signals to recover from a spoofing attack. Conclusions A new prototype GNSS spoofing detection system has been developed and tested using live-signal spoofing attacks. The system detects spoofing by using differences in signal direction-of-arrival characteristics between the spoofed and non-spoofed cases as sensed by a pair of GNSS antennas. A spoofing detection statistic has been developed that equals the difference between the optimized values of the negative-log-likelihood cost functions for two data-fitting problems. One problem fits the single-differenced beat carrier phases of multiple received signals to a spoofed model in which the fractional parts of these differences are identical -— in the absence of receiver noise — because the spoofed signals all arrive from the same direction. The other problem fits the single-differenced carrier phases to a non-spoofed model. This second optimal data-fitting problem is closely related to CDGPS attitude determination. The simple difference of the two optimized cost functions equals a large positive number if there is no spoofing, but it equals a negative number if the signals are being spoofed. Monte Carlo analysis of the probability distributions of this difference under the spoofed and non-spoofed assumptions indicates that it provides a powerful spoofing detection test with a low probability of false alarm. A real-time version of this system has been implemented using USRPs and real-time software radio receivers, and it has been tested against live-signal spoofing attacks aboard a yacht that was cruising around Italy. Successful detections have been achieved in many spoofing attack scenarios, and detections can occur in as little as 0.4 seconds or less. One scenario spoofed the yacht’s GPS receiver into believing that it had veered off of a northwesterly course towards Venice in the Adriatic to a southwesterly course towards the coast of Libya, and at the incredible speed of 900 knots. The spoofing detector, however, warned the crew on the bridge about the attack before the yacht’s spoofed position was 50 meters away from its true position. The live-signal tests revealed some challenges for this spoofing detection strategy. They occur primarily during the initial attack phase, before the spoofer has dragged the victim receiver to a wrong position or timing fix. If the spoofer power is not much larger than that of the true signals, then beating occurs between the spoofed and true signals during this initial period. This beating can cause difficulties for the receiver tracking loops, making single-differenced carrier phase unavailable. Even when single-differenced phase is available, both the spoofed and non-spoofed models of this quantity can be inadequate for purposes of designing a reliable spoofing detection test. This article’s new two-antenna spoofing detection system has generated promising real-time results against live-signal spoofing attacks, but further developments are needed to produce a sufficiently reliable detection system for all anticipated attack scenarios. The best defense will likely employ a multi-layered approach that uses the techniques described in this paper along with advanced RAIM techniques that detect additional signal anomalies that are characteristic of spoofing. Acknowledgments The authors (brief bios given in online version) thank the owner of the White Rose of Drachs for the loan of his vessel to conduct the live-signal GNSS spoofing detection tests reported here. The crew of the White Rose aided and supported this project in many ways. Red Team, White Team, Blue Team Background Before March 2013, members of the UT Radionavigation Lab and the Cornell GPS Lab didn’t know about gold-plated sinks and spiral staircases at sea. They did know something about spoofing navigation systems and detecting spoofer attacks. The UT group had hacked a helicopter drone at White Sands Missile Range in June 2012, coaxing it to dive towards the ground. The Cornell group had developed a prototype system that could reliably detect all UT Austin attacks, but it was clumsy, having an oscillating antenna and requiring hours of post-processing. Andrew Schofield, master of the White Rose of Drachs, attended Todd Humphreys’ 2013 South-by-Southwest conference talk on the drone hack and challenged him to go big — bigger than a 1.3-meter drone helicopter. How about a 65-meter superyacht? The result: a summer 2013 Mediterranean cruise that produced intriguing, provocative results. The UT team had implemented a feedback controller for their spoofer, but they were unable to control the spoofed drone in a smooth, reliable manner. The White Rose cruise offered a chance to test a next level of sophistication: a controlled sequence of lies leading the victim on a precise course selected by the spoofer, different from the one intended by the captain. The UT team was able to induce inadvertent turns while the ship’s bridge thought it was steering a straight course. They could nudge the yacht onto a wrong course paralleling the desired course. The crew remained unaware of the yacht’s true course because its GPS receiver and GPS-driven charts indicated that she was on her intended route. The Push for Protection Andrew Schofield quickly began advocating for a follow-up experiment: a UT Red Team attack against the White Rose GPS and a simultaneous Cornell Blue Team demonstration of real-time spoofing detection. The Cornell Team, however, faced challenges in transitioning from its initial prototype to a more sophisticated system, one that eliminated the moving parts and that operated in real time. Team members thought they could produce the next system, but had never been quite sure they could make good on their boast. Development of a second prototype system began with implementation of a new Cornell detection algorithm in Matlab. The first tests of this algorithm involved UT recording and pre-processing of transmissions in an RF chamber that housed the two antennas of Cornell’s second prototype. Cornell applied its new Matlab algorithm to these data and demonstrated off-line spoofing detection. The remaining hurdle was real-time operation. The original development plan called for translation of the Matlab algorithm to C++ followed by integration with a UT Austin/Cornell real-time software radio. It would be understatement to say that this was an ambitious task for the two-month window that remained until the White Rose cruise. UT Ph.D. student Jahshan Bhatti steered the team around this hurdle by proposing the direct use of Cornell’s Matlab code in the real-time system. Prior to this, no one had realized that it could be practical to call Matlab from C++ in real time. Mark Psiaki packaged the Matlab spoofing detection software into a single tic function, Jahshan coded the calling C++/Matlab interface, and the team was on track to test spoofing detection in late June 2014. Spoofer, Detector Clash at Sea The White Rose would sail from southern France on June 26, setting a course around Italy to Venice. The Cornell Blue Team would have three full days in international waters to demonstrate and evaluate their real-time spoofng detection system. A Ph.D. graduate from UT’s Radionavigation Laboratory would operate the Red Team spoofer, aka the Texas Lying Machine. In preparation for the voyage, the two teams converged in the White Roses’s home port of Cap-d’Ail. They performed initial shake-down tests of their systems in port. They could not do full live-signal tests in Cap d’Ail because they were still in French territorial waters. Transmission of live spoofing signals in the GPS L1 band is permitted only in international waters, and only if conducted for scientific purposes. The spoofing and detection tests started in earnest on the morning of June 27 off the southern coast of Italy. The White Rose had passed through the Strait of Messina between Italy and Sicily earlier that day. The initial tests were concerned with antenna geometries and spoofer power levels. Later tests concentrated on serious deception of the White Rose regarding its true course and location. During the tests, the UT Red team and its spoofer were situated on the White Rose Sun Deck, above and behind the bridge. The Cornell Blue team and its electronics were on the bridge with its two antennas on the roof. A walkie-talkie link between the teams provided coordination of detector operation with spoofing attacks along with feedback about spoofer and detector performance. Hijacked to Libya! For the final day of tests, Andrew Schofield suggested sending the spoofed White Rose to Libya as she cruised the Adriatic from Montenegro to Venice — a difference of 600 nautical miles. The target trip time of 50 minutes necessitated a peak speed over 900 knots (1,667 kilometers/hour) after factoring the need to limit initial acceleration and final deceleration; if too large, they might cause the victim receiver’s tracking loops to lose lock and, therefore, the spoofed signals. The Cornell and UT Austin teams programmed the spoofer for a trip to Libya, and they initiated the attack. The White Rose bridge soon became a scene of excitement. The ship started veering sharply to port, and its velocity vector lengthened until it literally went off the charts. The GPS receiver showed the ship hurrying towards Libya on a collision course with the back of Italy’s boot. The bridge’s GPS receiver displayed speeds that increased through 100 knots, 200 knots, 300 knots — for a yacht with a speed capability of about 15 knots. The Cornell detector issued a spoofing alert at the onset of the attack, long before the White Rose veered off course. After a few minutes, the detector’s continued successful operation became boring. Of course, boring success is better than exciting failure. The Cornell system had not been as successful during some of the preceding attacks, and the results from the June voyage suggested avenues for improvement. If new live-signal tests become necessary to evaluate planned improvements, the Red and Blue teams stand ready for a future superyacht cruise. See http://blogs.cornell.edu/yachtspoof for further details. Mark L. Psiaki is a Professor of Mechanical and Aerospace Engineering. He received a B.A. in Physics and M.A. and Ph.D. degrees in Mechanical and Aerospace Engineering from Princeton University. His research interests are in the areas of GNSS technology and applications, spacecraft attitude and orbit determination, and general estimation, filtering, and detection. Brady W. O’Hanlon is a graduate student in the School of Electrical and Computer Engineering. He received a B.S. in Electrical and Computer Engineering from Cornell University. His interests are in the areas of GNSS technology and applications, GNSS security, and space weather. Steven P. Powell is a Senior Engineer with the GPS and Ionospheric Studies Research Group in the Department of Electrical and Computer Engineering at Cornell University. He has M.S. and B.S. degrees in Electrical Engineering from Cornell University. He has been involved with the design, fabrication, testing, and launch activities of many scientific experiments that have flown on high altitude balloons, sounding rockets, and small satellites. He has designed ground-based and space-based custom GPS receiving systems primarily for scientific applications. Jahshan A. Bhatti is pursuing a Ph.D. in the Department of Aerospace Engineering and Engineering Mechanics at the University of Texas at Austin, where he also received his M.S. and B.S. He is a member of the UT Radionavigation Laboratory. His research interests are in the development of small satellites, software-defined radio applications, space weather, and GNSS security and integrity. Todd E. Humphreys is an assistant professor in the department of Aerospace Engineering and Engineering Mechanics at the University of Texas at Austin, and Director of the UT Radionavigation Laboratory. He received a B.S. and M.S. in Electrical and Computer Engineering from Utah State University and a Ph.D. in Aerospace Engineering from Cornell University. He specializes in applying optimal estimation and signal processing techniques to problems in radionavigation. His recent focus is on radionavigation robustness and security. Andrew Schofield is a career Yacht Captain. After completing his degree in Applied Biology and working in the bio-science industry for a year, he left all that behind in 1991 and found a deck hand’s job on a sailing yacht in the Caribbean. Since then he has worked on various yachts in various locations. He has been Captain of the White Rose of Drachs since launch in June 2004. He is President of the Professional Yachting Association, the large yacht professional body, and focuses on the training and certification of crew. In his time at sea GPS has transformed navigation. He feels that the relevance of the work done to detect GPS spoofing cannot be overstated with regard to the safety of life at sea, and he is delighted to have facilitated the voyage during which spoofing detection was proven.
blocking phone
Samsung tad437 jse ac adapter 5vdc 0.7a used.travel charger powe.or even our most popular model,the world’s largest social music platform.atc-frost fps2016 ac adapter 16vac 20va 26w used screw terminal.whether copying the transponder.cincon tr36a-13 ac adapter 13.5v dc 2.4a power supply,disrupting the communication between the phone and the cell-phone base station.replacement lac-mc185v85w ac adapter 18.5vdc 4.6a 85w used,usually by creating some form of interference at the same frequency ranges that cell phones use.aopen a10p1-05mp ac adapter 22v 745ma i.t.e power supply for gps.micro controller based ac power controller.57-12-1200 e ac adapter 12v dc 1200ma power supply,anoma electric aec-t5713a ac adapter 13.5vdc 1.5a power supply,dell adp-lk ac adapter 14vdc 1.5a used -(+) 3x6.2mm 90° right.sadp-65kb b ac switching adapter 19v 1.58a -(+)- 1.8x5mm used 10,fsp fsp050-1ad101c ac adapter 12vdc 4.16a used 2.3x5.5mm round b,motorola ssw-0828 ac adapter 6.25v 350ma cell phone chargercon.a low-cost sewerage monitoring system that can detect blockages in the sewers is proposed in this paper,blackberry bcm6720a battery charger 4.2vdc 0.7a used 100-240vac~.nikon eh-69p ac adapter 5vdc 0.55a used usb i.t.e power supply 1.ac-5 41-2-15-0.8adc ac adapter 9vdc 850 ma +(-)+ 2x5.5mm 120vac,browse recipes and find the store nearest you.khu045030d-2 ac adapter 4.5vdc 300ma used shaver power supply 12,skynet dnd-3012 ac adapter 30vdc 1a used -(+)- 2.5x5.5mm 120vac.hon-kwang hk-a112-a06 ac adapter 6vdc 0-2.4a used -(+) 2.5x5.5x8,hppa-1121-12h ac adapter 18.5vdc 6.5a 2.5x5.5mm -(+) used 100-,frequency counters measure the frequency of a signal,altec lansing mau48-15-800d1 ac adapter 15vdc 800ma -(+) 2x5.5mm.kec35-3d-0.6 ac adapter 3vdc 200ma 0.6va used -(+)- 1 x 2.2 x 9..replacement dc359a ac adapter 18.5v 3.5a used 2.3x5.5x10.1mm.ryobi p113 ac adapter 18vdc used lithium ion battery charger p10,fujitsu ac adapter 19vdc 3.68 used 2.8 x 4 x 12.5mm.Nokia acp-7e ac adapter 3.7v 355ma 230vac chargecellphone 3220,replacement pa-1700-02 ac adapter 20vdc 4.5a used straight round,jobmate battery charger 18vdc used for rechargeable battery.which broadcasts radio signals in the same (or similar) frequency range of the gsm communication.hr-091206 ac adapter 12vdc 6a -(+) used 2.4 x 5.4 x 12mm straigh.motorola dch3-05us-0300 travel charger 5vdc 550ma used supply.ktec ksas0241200150hu ac adapter12v dc 1.5a new -(+) 2.5x5.5x1.sony ac-64na ac adapter 6vdc 400ma used -(+)- 1.8x4x9.7mm,sharp ea-51a ac adapter 6vdc 200ma usedstraight round barrel p,apx141ps ac dc adapter 15v dc 1500ma power supply,5vdc 500ma ac adapter used car charger cigarate lighter 12vdc-24.hp 0950-3796 ac adapter 19vdc 3160ma adp-60ub notebook hewlett p,the pki 6025 is a camouflaged jammer designed for wall installation.pa-1650-02h replacement ac adapter 18.5v 3.5a for hp laptop powe.canon ad-50 ac adapter -(+)- +24vdc 1.8a used 2x5.5mm straight r,car charger 12vdc 550ma used plug in transformer power supply 90.apple a1021 ac adapter 24vdc 2.65a desktop power supply power bo.ac adapter 6vdc 3.5a 11vdc 2.3a +(-)+ 2.5x5.5mm power supply.nextar fj-t22-1202500v ac adapter 12v 250ma switching power supp.ad-90195d replacement ac adapter 19.5v dc 4.62a power supply,chang zhou tai yu rkdc0450300 ac adapter 4.5vdc 300ma power supp,if you are looking for mini project ideas,lei mt15-5050200-a1 ac adapter 5v dc 2a used -(+) 1.7x4x9.4mm,kyocera txtvl0c01 ac adapter 4.5v 1.5a travel phone charger 2235,ast ad-4019 eb1 ac adapter 19v 2.1a laptop power supply,this break can be as a result of weak signals due to proximity to the bts.tongxiang yongda yz-120v-13w ac adapter 120vac 0.28a fluorescent,superpower dv-91a-1 ac adapter 9vdc 650ma used 3 pin molex direc,yj yj-502
Advent 35-12-200c ac dc adapter 12v 100ma power supply,it is convenient to open or close a ….impediment of undetected or unauthorised information exchanges,hon-kwang d7-10 ac adapter 7.5vdc 800ma used -(+) 1.7x5.5x12mm 9,the electrical substations may have some faults which may damage the power system equipment.black & decker fs18c 5103069-12 ac adapter 21.75v dc 210ma used.925 to 965 mhztx frequency dcs.delta eadp-25bb a ac adapter 5v 5a laptop power supply,finecom hk-a310-a05 uk 510 charger 5vdc 3a +(-) 2x5.5mm replacem,generation of hvdc from voltage multiplier using marx generator.single frequency monitoring and jamming (up to 96 frequencies simultaneously) friendly frequencies forbidden for jamming (up to 96)jammer sources.video digitial camera travel battery charger.creative dv-9440 ac adapter 9v 400ma power supply.motorola psm5049a ac adapter dc 4.4v 1.5a cellphone charger,cell phone jammer is an electronic device that blocks transmission of signals …,nec pa-1700-02 ac adapter 19vdc 3.42a 65w switching power supply,motorola spn4226a ac adapter 7.8vdc 1a used power supply,shanghai dy121-120010100 ac adapter 12v dc 1a used -(+) cut wire,are suitable means of camouflaging,this device can cover all such areas with a rf-output control of 10.arduino are used for communication between the pc and the motor,zhongshan p1203e ac adapter 12vdc 2a used -(+) 2x5.5x9mm round b.belkin utc001-b usb power adapter 5vdc 550ma charger power suppl,the paralysis radius varies between 2 meters minimum to 30 meters in case of weak base station signals.southwestern bell 9a200u-28 ac adapter 9vac 200ma 90° right angl,
,aw17-3r3-u ac adapter 3.3vdc 5a used 1.8x5.5x9.7mm straight.nokia ac-15x ac adapter cell phone charger 5.0v 800ma europe 8gb,bell phones u090050d ac dc adapter 9v 500ma class 2 power supply,pega nintendo wii blue light charge station 300ma.potrans up04821120a ac adapter 12vdc 4a used -(+) 2x5.5x9.7mm ro,circut ksah1800250t1m2 ac adapter 18vdc 2.5a 45w used -(+) 2.2x5.Hp 384021-001 compaq ac adapter 19vdc 4.7a laptop power supply.ibm lenovo 92p1020 ac adapter 16vdc 4.5a used 2.5x5.5mm round ba,main business is various types of jammers wholesale and retail,zte stc-a22o50u5-c ac adapter 5vdc 700ma used usb port plug-in d,thus it was possible to note how fast and by how much jamming was established,dve dsa-12pfa-05 fus 050200 ac adapter +5vdc 2a used -(+) 0.5x2x,the systems applied today are highly encrypted.dragon sam-eaa(i) ac adapter 4.6vdc 900ma used usb connector swi,basically it is way by which one can restrict others for using wifi connection,tiger power tg-6001-12v ac adapter 12vdc 5a used 3 x 5.5 x 10.2.jvc aa-v15u ac power adapter 8.5v 1.3a 23w battery charger,pa-1600-07 replacement ac adapter 19vdc 3.42a -(+)- 2.5x5.5mm us,toshiba pa-1121-04 ac dc adapter 19v 6.3a power supplyconditio,anoma abc-6 fast battery charger 2.2vdc 1.2ahx6 used 115vac 60hz,the scope of this paper is to implement data communication using existing power lines in the vicinity with the help of x10 modules,nokiaacp-12x cell phone battery uk travel charger,philips hq 8000 ac adapterused charger shaver 100-240v 50/6.this project uses arduino and ultrasonic sensors for calculating the range,electra 26-26 ac car adapter 6vdc 300ma used battery converter 9,2110 to 2170 mhztotal output power.codi a03002 ac adapter 20vac 3.6a used 3 pin square auto/air pow,oral-b 3733 blue charger personal hygiene appliance toothbrush d.law-courts and banks or government and military areas where usually a high level of cellular base station signals is emitted,atlinks usa inc. 5-2509 ac dc adapter 9v 450ma 8w class 2 power.soneil 2403srd ac adapter 24vdc 1.5a 3pin xlr connector new 100-,archer 273-1652a ac adapter 12vdc 500ma used -(+) 2x5.5mm round,kodak mpa7701 ac adapter 24vdc 1.8a easyshare dock printer serie.imex 9392 ac adapter 24vdc 65ma used 2 x 5.5 x 9.5mm,pure energy ev4-a ac adapter 1.7vdc 550ma used class 2 battery c.ac adapter 5.2vdc 450ma used usb connector switching power supp,hi capacity le-9720a-05 ac adapter 15-17vdc 3.5a -(+) 2.5x5.5mm,here is the diy project showing speed control of the dc motor system using pwm through a pc.
Sanyo scp-14adt ac adapter 5.1vdc 800ma 0.03x2mm -(+) cellphone,frequency band with 40 watts max,mintek adpv28a ac adapter 9v 2.2a switching power supply 100-240,cisco wa15-050a ac adapter +5vdc 1.25a used -(+) 2.5x5.5x9.4mm r,texas instruments xbox 5.1 surround sound system only no any thi,sps15-12-1200 ac adapter 12v 1200ma direct plug in power supply.230 vusb connectiondimensions,asian power devices inc da-48h12 ac dc adapter 12v 4a power supp.ault a0377511 ac adapter 24v 16va direct plugin class2 trans pow,portable personal jammers are available to unable their honors to stop others in their immediate vicinity [up to 60-80feet away] from using cell phones,battery charger for hitachi dvd cam dz-bx35a dz-acs3 ac new one.hp pa-1900-15c1 ac adapter 18.5vdc 4.9a 90w used,fujitsu sq2n80w19p-01 ac adapter 19v 4.22a used 2.6 x 5.4 x 111.,atlinks 5-2418 ac adapter 9vac 400ma ~(~) 2x5.5mm 120vac class 2,asus pa-1650-02 ac adapter 19vdc 3.42a 65w used -(+)- 2.5x5.4mm,ault t57-182200-j010g ac adapter 18v ac 2200ma used,health o meter adpt25 ac adapter 6v dc 300ma power supply.dve dsa-0251-05 ac adapter 5vdc 5a used 2.5x5.5x9mm 90 degree,energizer fps005usc-050050 ac adapter 5vdc 0.5a used 1.5x4mm r,yamaha pa-1210 ac adapter 12vdc 1a used -(+) 2x5.5x10mm round ba.this project shows the control of home appliances using dtmf technology.sanyo var-l20ni li-on battery charger 4.2vdc 650ma used ite powe.globtek gt-4076-0609 ac adapter 9vdc 0.66a -(+)- used 2.6 x 5.5,compaq pp2012 ac adapter 15vdc 4.5a 36w power supply for series.including almost all mobile phone signals,au35-030-020 ac adapter 3vdc 200ma e144687 used 1x3.2mm round ba,sun pscv560101a ac adapter 14vdc 4a used -(+) 1x4.4x6mm samsung,the effectiveness of jamming is directly dependent on the existing building density and the infrastructure,71109-r ac adapter 24v dc 500ma power supply tv converter.motorola psm5037b travel charger 5.9v 375ma ac power supply spn5.walker 1901.031 ac adapter 9vdc 100ma used -(+) 2.1x5.3mm round,campower cp2200 ac adapter 12v ac 750ma power supply.
Ad-0815-u8 ac adapter 7.5vdc 150ma used -(+)- 4.5 x 5.6 x 9 mm 2.solar energy measurement using pic microcontroller,sino-american sa120a-0530v-c ac adapter 5v 2.4a new class 2 powe,hi capacity ac-c10 le 9702a 06 ac adapter 19vdc 3.79a 3.79a 72w,apd wa-10e05u ac adapter 5vdc 2a used 1.8x4mm -(+) 100-240vac,panasonic cf-aa1653a ac adapter 15.6vdc 5a ite power supply cf-1,prudent way pw-ac90le ac adapter 20vdc 4.5a used -(+) 2x5.5x12mm.oem ad-2430 ac adapter 24vdc 300ma used -(+) stereo pin plug-in.air rage wlb-33811-33211-50527 battery quick charger.the operating range is optimised by the used technology and provides for maximum jamming efficiency,intertek bhy481351000u ac adapter 13.5vdc 1000ma used -(+) 2.3x5.acbel api3ad03 ac adapter 19v dc 3.42a toshiba laptop power supp.cc-hit333 ac adapter 120v 60hz 20w class 2 battery charger,new bright a865500432 12.8vdc lithium ion battery charger used 1.asus exa0901xh ac adapter 19v 2.1a power supply laptop.this device is a jammer that looks like a painting there is a hidden jammer inside the painting that will block mobile phone signals within a short distance (working radius is 60 meters),thermo gastech 49-2163 ac adapter 12.6vdc 220/70ma battery charg.handheld drone jamming gauge sc02,lp-60w universal adapter power supply toshiba laptop europe,cui 3a-501dn09 ac adapter 9v dc 5a used 2 x 5.5 x 12mm,motorola psm4250a ac adapter 4.4vdc 1.5a used cellphone charger,mascot 2415 ac adapter 1.8a used 3 pin din connector nicd/nimh c,50/60 hz permanent operationtotal output power,duracell cef15adpus ac adapter 16v dc 4a charger power cef15nc,altec lansing s024eu1300180 ac adapter 13vdc 1800ma -(+) 2x5.5mm,gamestop bb-731/pl-7331 ac adapter 5.2vdc 320ma used usb connect.intermatic dt 17 ac adapter 15amp 500w used 7-day digital progra,gateway li shin lse0202d1990 ac adapter 19vdc 4.74a used 2.5 x 5.toshiba pa3201u-1aca ac adaptor 15v 5a 1800 a50 5005 m5 r200 lap,yh-u35060300a ac adapter 6vac 300ma used ~(~) 2x5.5mm straight r,boss psa-120t ac adapter 9.6vdc 200ma +(-) 2x5.5mm used 120vac p,computer wise dv-1280-3 ac adapter 12v dc 1000ma class 2 transfo.
Fujitsu fmv-ac316 ac adapter 19vdc 6.32a used center +ve 2.5 x 5.remington pa600a ac dc adapter 12v dc 640ma power supply,delta adp-90cd db ac adapter 19vdc 4.74a used -(+)- 1.5x5.5x11mm,hp 0950-3195 ac adapter 5vdc 3a 3.3vdc 1.6a 8pin power supply,in common jammer designs such as gsm 900 jammer by ahmad a zener diode operating in avalanche mode served as the noise generator,set01b electronic transformer 12vac 105w 110vac crystal halogen,ps06b-0601000u ac adapter used -(+) 6vdc 1000ma 2x5.5mm round ba.lenovo 41r4538 ultraslim ac adapter 20vdc 4.5a used 3pin ite,apx technologies ap3927 ac adapter 13.5vdc 1.3a used -(+)- 2x5.5,aps aps48ea-114 ac dc adapter 7.5v 1.5a power supply,motorola aa26100l ac adapter 9vdc 2a -(+)- 1.8x4mm used 1.8 x 4,canon cb-2lwe ac adapter 8.4vdc 0.55a used battery charger,aps ad-740u-1120 ac adapter 12vdc 3a used -(+)- 2.5x5.5mm barrel.compaq series 2872 ac adapter 18.75vdc 3.15a 41w91-55069,the integrated working status indicator gives full information about each band module,panasonic de-891aa ac adapter 8vdc 1400ma used -(+)- 1.8 x 4.7 x.oem ads0248-w 120200 ac adapter 12v dc 2a used -(+)- 2.1x5.5mm,hoover series 500 ac adapter 8.2vac 130ma used 2x5.5x9mm round b,sony ac-l200 ac adapter 8.4vdc 1.7a camcorder power supply.mw41-1200600 ac adapter 12vdc 600ma used -(+) 2x5.5x9mm round ba.rexon ac-005 ac adapter 12v 5vdc 1.5a 5pin mini din power supply.in case of failure of power supply alternative methods were used such as generators,meikai pdn-48-48a ac adapter 12vdc 4a used -(+) 2x5.5mm 100-240v.netmask is used to indentify the network address,71109-r ac adapter 24v dc 350ma power supply tv converter used.konica minolta bc-600 4.2v dc 0.8a camera battery charger 100-24,creative sw-0920a ac adapter 9vdc 2a used 1.8x4.6x9.3mm -(+)- ro,aastra m8000 ac adapter 16vac 250ma ~(~) 2.5x5.5m,2 ghzparalyses all types of remote-controlled bombshigh rf transmission power 400 w.thomson 5-2752 telephone recharge cradle with 7.5v 150ma adapter,chicony a11-065n1a ac adapter 19vdc 3.42a 65w used -(+) 1.5x5.5m,cyber acoustics ac-8 ca rgd-4109-750 ac adapter 9vdc 750ma +(-)+.
Gps signal blocker jammer network,lac-cp19v 120w ac adapter 19v 6.3a replacement power supply comp,le-9702b ac adapter 12vdc 3.5a used -(+) 4pin din lcd power supp,braun 4729 ac adapter 250vac ~ 2.5a 2w class 2 power supply,the light intensity of the room is measured by the ldr sensor.ibm 85g6704 ac adapter 16v dc 2.2a power supply 4pin 85g6705 for,hh-stc001a 5vdc 1.1a used travel charger power supply 90-250vac,jabra acw003b-05u ac adapter 5v 0.18a used mini usb cable supply,liteon pa-1750-08 ac adapter 15vdc 5a pa3378u-1aca pa3378e-1aca.canon a20630n ac adapter 6vdc 300ma 5w ac-360 power supply,as many engineering students are searching for the best electrical projects from the 2nd year and 3rd year.868 – 870 mhz each per devicedimensions.databyte dv-9200 ac adapter 9vdc 200ma used -(+)- 2 x 5.5 x 12 m.ktec ksaa0500120w1us ac adapter 5vdc 1.2a new -(+)- 1.5x4mm swit,the proposed system is capable of answering the calls through a pre-recorded voice message,at am0030wh ac adapter used direct plug involtage converter po,liteon pa-1750-11 ac adapter -(+)- 19vdc 4a used 2.7x5.4mm.liteon pa-1041-71 ac adapter 12vdc 3.3a used -(+) 2x5.5x9.4mm ro..